Airbus A320-232

Service difficulty reports · 32,653

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A320232'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR YENA201807020264Battery · dischargedDURING HEAVY MAINTENANCE, EMERGENCY LIGHT FAIL MESSAGE "EPSU INT LOAD FWD L" AND "EPSU ARMED / ON AFT L" DURING PTP TEST; REMOVED AND REPLACED EPSU 13WL IAW AMM 32-51-38. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-38. RE-TERMINATED PIN C OF 13WL-A CONNECTJun 26, 2018 · N568JB · Airbus A320232 · Emergency LightingSDR AALA201806279008Seal · damagedFIRST OFFICER'S WINDSHIELD HAD A DAMAGED SEAL. REPLACED THE WINDSHIELD IAW AMM 56-11-11.Jun 26, 2018 · N647AW · Airbus A320232 · Flight Compartment WindowsSDR YENA201806250927Pressure Panel · crackedDURING HEAVY MAINTENANCE, SEVERAL CRACKS WERE FOUND. REFER TO EC A18-504-01. FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36 / LT & RT SIDES / PRESSURE PANEL ATTACHMENT HOLES / CRACK DAMAGE - PERMANENT REPAIR; THIS TIME LIMITED REPAIR HAS BEEN APPROVEDJun 25, 2018 · N508JL · Airbus A320232 · Fuselage Main, BulkheadSDR YENA201806250926Window Post · crackedDURING CURRENT (6/2018) C10 HEAVY CHECK AT SAL, UNDERGOING REF /3/ INSPECTION WHEN A CRACK WAS FOUND ON WINDSHIELD LT SIDE POST UPPER SECTION AT FR4 (SEE REF /1/ EA FOT DETAILS). WITHOUT ANY SRM REPAIR OPTIONS, CONTACTED AND PROVIDED REF /4/ REPAIR DRAWING. THJun 25, 2018 · N508JL · Airbus A320232 · Fuselage Main, StructureSDR CALA2018071001583Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 32 BETWEEN STRINGER 43 AND 44 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR32 STR43-44L NOMINAL THICKNE SS .055" MATERIAL LOSS .008" REMAINING MATERIAL .047" ALLOWABLE LOSS .004" FOUND TO BE OUT OF LIMITS IAW SMJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001582Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 26 BETWEEN STRINGER 42 AND 4 3 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR26 STR42-43L NOMINAL THICKNESS .055" MATERIAL LOSS .005" REMAINING MATERIAL .49" ALLOWABLE LOSS .004" FOUND TO BE OUT OF LIMITS IAW SM Jun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071101598Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 31 BETWEEN STRINGER 43 AND 44 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR31 STR43-44L NOMINAL THICKNESS .055" MATERIAL LOSS .009" REMAINING MATERIAL .046" ALLOWABLE LOSS .004" IAW SM ASNA3042. REMOVED AND REPLJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071101597Shear Tie · corrodedFORWARD CARGO COMP FRAME 31 BETWEEN STRINGER 39 AND 40 RIGHT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR31 STR39-40R NOMINAL THICKNESS .055" MATERIAL LOSS .020" REMAINING MATERIAL .055 ALLOWABLE MINIMUM REMAINING THICKNESS .039" FOUND TO BE OUT OFJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071101596Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 32 BETWEEN STRINGER 41 AND 4 2 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE FR32 STR41-42L ORIG THICKNESS .05 5 LOSS. 007 REMAINING .048 ALLOWABLE LOSS .004 OUT OF LIMITS IAW SM ASNA3042. REMOVED AND REPLACED SHEAR TIJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071101595Shear Tie · corrodedFORWARD C ARGO COMPARTMENT FRAME 30 BETWEEN STRINGER 41 AND 42 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR30 STR41-42L NOMINAL THICKNESS .055" MATERIAL LOSS .013" REMAINING MATERIAL .042" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SMJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001594Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 32 BETWEEN STRINGER 40 AND 41 RIGHT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE FR32 STR40-41R NOMINAL THICKNESS .055" MATERIAL LOSS .005" REMAINING MATERIAL .050" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001593Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 33 BETWEEN STRINGER 41 AND 42 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR33 STR41-42L NOMINAL THICKNESS .055" MATERIAL LOSS .006" REMAINING MATERIAL .049" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM Jun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001592Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 26 BETWEEN STRINGER 42 AND 4 3 SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR26 STR44-43R NOMINAL THICKNESS .055" MATERIAL LOSS .018" REMAINING MATERIAL .037" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNAJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001591Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 30 BETWEEN STRINGER 42 AND 4 3 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR30 STR42-43L NOMINAL THICKNESS .055" MATERIAL LOSS .006" REMAINING MATERIAL .049" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SMJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001590Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 29 BETWEEN STRINGER 43 AND 44 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR29 STR44-43L NOMINAL THICKNESS .055" MATERIAL LOSS .007" REMAINING MATERIAL .048" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SRMJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001589Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 30 BETWEEN STRINGER 40 AND 41 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR30 STR40-41L NOMINAL THICKNESS .055" MATERIAL LOSS .008" REMAINING MATERIAL .047", ALLOWABLE LESS .004" FOUND TO BE OUT OF LIMITS IAW SM Jun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001588Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 32 BETWEEN STRINGER 42 AND 4 3 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE ON FR32 STR42-43 NOMINAL THICKNESS .055" MATERIAL LOSS .007" REMAINING MATERIAL .048" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM Jun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001587Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 29 BETWEEN STRINGER 40 AND STRINGER 41 LEFT CORRODED SHEAR TIE. BLENDED CORROSION ON SHEAR TIE FR29 STR40-41L NOMINAL THICKNESS .055" MATERIAL LOSS .006" REMAINING MATERIAL .040" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001586Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 29 BETWEEN STRINGER 42 AND 4 3 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR29 STR42-43L NOMINAL THICKNESS .055" MATERIAL LOSS .015" REMAINING .040" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042Jun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001585Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 31 BETWEEN 42 AND 43 LEFT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR31 STR42-43L NOMINAL THICKNESS .055" MATERIAL LOSS .008" REMAINING MATERIAL .047" ALLOWABLE LOSS .004", FOUND TO BE OUT OF LIMITS IAW SM ASNA3042.Jun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001584Shear Tie · corrodedFORWARD CARGO COMPARTMENT FRAME 32 BETWEEN STRINGER 41 AND 4 2 RIGHT SHEAR TIE CORRODED. BLENDED CORROSION ON SHEAR TIE AT FR32 STR41-42R .055" NOMINAL THICKNESS MATERIAL LOSS .010" REMAINING MATERIAL .045" ALLOWABLE REMAINING MINIMUM THICKNESS .051", FOUND TOJun 25, 2018 · N421UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2018071001580Intercostal · crackedRT FWD PAX DOOR NR 1 DOOR STOP FITTING LOWER I/B FASTENER HOLE HAS CRACK INDICATION. REMOVED NR 1 DOOR STOP FITTING, REMOVED AND REPLACED DAMAGED INTERCOSTAL AT RT FWD PAX DOOR FR16 IAW ECRA 5311-01961, INSTALLED NR 1 DOOR STOP FITTING IAW AMM 52-11-31-000-002Jun 25, 2018 · N432UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201806299003Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE. BUSHING BORE WORN ON LEFT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING BETWEEN STA 42 TO STA 43, WATERLINE Z-2166, LBL Y254 ON KEEL BEAM. REPLACED LEFT HAND MAIN LANDING GEAR DOOR HINGE FITTING PER EA 281727 AND REPAIR DRAWING R53Jun 25, 2018 · N647AW · Airbus A320232 · Landing Gear DoorsSDR AALA201806299002Intercostal · crackedAIRCRAFT WAS IN BASE MAINTENANCE. CRACK INDICATED ON LOWER INBOARD HOLE IN INTERCOSTAL FOR RIGHT DOOR STOP FITTING NR 1. REPLACED INTERCOSTAL PER DRAWING D53112300, AND DRAFT EA 281693Jun 25, 2018 · N647AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201806240925Skin · dentedDURING CURRENT (6/2018) C7 HEAVY CHECK AT LHT-PR, REPORTED WITH A DENT AT REAR FUSELAGE BETWEEN FR 63 AND 64, STGR 4L AND 5L MEASURING 67MM L X 46MM W X 2.6MM D (SEE REF /1/ EO FOR DETAILS). THIS AREA IS CLASSIFIED AS AN EXLUDED AREA WITHOUT REPAIR ALLOWANCES,Jun 24, 2018 · N623JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR AALA201807029034Attach Fitting · crackedRIGHT MLG DOOR ACTUATOR AFT ATTACH FITTING ON KEEL BEAM HAS A CRACK INDICATION IN RADIUS BELOW ACTUATOR ATACHMENT BORE. REPLACED RIGHT MLG DOOR ACTUATOR ATTACH FITTING IAW SRM 51-72-11, EA 281899 AND REPAIR DRAWING R53370501.Jun 24, 2018 · N647AW · Airbus A320232 · Fuselage Main, Attach FittingsSDR AALA201807029033Attach Fitting · crackedLEFT MAIN LANDING GEAR DOOR ACTUATOR AFT ATTACH FITTING HAS A CRACK INDICATION IN THE RADIUS BELOW ACTUATOR ATTACHMENT. REPLACED THE FITTING IAW EA 281898.Jun 24, 2018 · N647AW · Airbus A320232 · Fuselage Main, Attach FittingsSDR AALA201806269034Battery · dischargedAIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT FLIGHT ATTENDANT INOPERABLE. MAINTENANCE REPLACED FORWARD OUTBOARD, FLIGHT ATTENDANT, FLASHLIGHT BATTERY PER AMM 25-60-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.Jun 24, 2018 · N601AW · Airbus A320232 · Emergency EquipmentSDR GTIA2018062532711Inlet · contaminatedDIRTY SOCKS ODOR. CLEANED HYD FLUID FROM THE APU INLET, PERFORMED AN OPS TEST OF CSAS IAW AMM 21-58-00. NO ODOR NOTED.Jun 23, 2018 · N635NK · Airbus A320232 · APU Core EngineSDR GTIA2018062532710Seal · leakingDURING GEAR EXTENSION, FA REPORTED A STRONG ODOR FROM THE VENTS. NR 1 PACK WAS OFF AT THE TIME IAW TSM 05-50-00-810-831-A. FOUND THE NR 2 ENGINE DE-OILER LEAKING. REMOVED & REPLACED THE NR 2 ENGINE DE-OILER SEAL IAW AMM 72-60-31.Jun 23, 2018 · N615NK · Airbus A320232 · Turbine Engine Oil SystemSDR CALA2018070301558Beam · corrodedLT AFT EMERGENCY EXIT DOOR CUTOUT. LOWER SURFACE BETWEEN THE LATCHES FOUND CORRODED AFTER CHECKING MATING SURFACE OF CORRODED HATCH. REMOVED CORRODED BEAM AT LT AFT EMERGENCY EXIT DOOR LOWER BEAM. MATCH DRILLED NEW BEAM AND INSTALLED NEW BEAM RESTORED SURFACE Jun 22, 2018 · N432UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018070301540Shear Plate · corrodedCABIN FR70 STR 23L SHEAR PLATE SUPPORT WEB CORRODED. REMOVED AND REPLACED SHEAR PLATE SUPPORT IAW SRM 51-42-11-0 01.Jun 22, 2018 · N1902U · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018070301542Stringer · corrodedAFT CARGO BAY STR 40L AT FR57 IS CORRODED. AFTER EVAL OF STR 40L AT FR57 TO FR58, FOUND STR 40L TO BE 100% MATERIAL LOSS. PERFORMED REPAIR IAW SRM 53-00-13-300-001, ER 5100R01017 REV E.Jun 22, 2018 · N455UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR GTIA2018062202709A/C Pack · odorPAX AND FA REPORTED AN ODOR IN CABIN WHILE TAXING OUT. TROUBLESHOT AND DETERMINED IT WAS THE NR 1 PACK. CONFIRMED THE NR 1 PACK WAS THE SOURCE OF ODOR.Jun 22, 2018 · N615NK · Airbus A320232 · Cabin Cooling SystemSDR CALA2018070301537Door Sill · corrodedR2 DOOR SILL HAS CORROSION ON INB OARD EDGE AT FR68. REPAIRED CORRODED AREA ON R2 DOOR SILL AT FR68 INBOARD EDGE IAW SRM 53-41-14-300-001 REPAIR PRINCIPLE 7.Jun 21, 2018 · N432UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018062210263Lens · missingRIGHT OVERWING EXIT, TWO EMERGENCY EXIT SIGN COVERS WERE MISSING. REPLACED THE COVERS IAW AMM 33-51-15. OPS CHECKED GOOD. ACFT OK FOR SERVICE.Jun 21, 2018 · N569JB · Airbus A320232 · Emergency LightingSDR YENA2018062210262Battery Pack · no testBATTERY PACKS 10WL, 11WL, AND 12WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY PACKS IAW AMM 33-51-38. CHECKED GOOD.Jun 21, 2018 · N638JB · Airbus A320232 · Emergency LightingSDR YENA2018062210261Battery Pack · no testBATTERY PACKS 10WL, 11WL, AND 12WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY PACKS IAW AMM 33-51-38. CHECKED GOOD.Jun 21, 2018 · N638JB · Airbus A320232 · Emergency LightingSDR YENA2018062210260Battery Pack · failedBATTERY PACKS 10WL, 11WL, AND 12WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY PACKS IAW AMM 33-51-38. CHECKED GOOD.Jun 21, 2018 · N638JB · Airbus A320232 · Emergency LightingSDR YENA2018062210259Light · inoperativeOVERWING DOOR EMERGENCY LIGHT INOPERATIVE, ESCAPE HATCH HANDLE LIGHT. REPLACED THE OVERWING DOOR ESCAPE HATCH EMERGENCY LIGHT IAW AMM 33-51-11.Jun 21, 2018 · N554JB · Airbus A320232 · Emergency LightingSDR CALA2018062201511Connector · damagedBROKEN CONNECTOR BACKSHELL AND DAMAGED WIRES ON THE EMERGENCY LIGHT WIRE HARNESS AT SEAT ROWS 23 - 25ABC. REMOVED AND REPLACED THE CONNECTOR BACKSHELL AND TERMINATED THE WIRES IAW ESPM 20-48-21-0011. OPS CHECKED GOOD.Jun 20, 2018 · N418UA · Airbus A320232 · Light System WiringSDR CALA2018062201510Hook · looseR1 DOOR INTERIOR HANDLE LOCKING HAMMER WAS LOOSE. ADJUSTED THE HANDLE LOCKING HAMMER HOOK IAW CMM 5 2-11-15, AND 52-11-15-400-048-A01.Jun 20, 2018 · N432UA · Airbus A320232 · Service DoorsSDR CALA2018062201509Hook · inoperativeL2 DOOR INERIOR HANDLE DID NOT LOCK. REMOVED AND REPLACED THE L2 DOOR INTERIOR HANDLE LOCK HOOK IAW CMM 52-13-15-400-054-A01.Jun 20, 2018 · N432UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2018062201508Hook · out of adjustL1 DOOR, INSIDE HANDLE DOES NOT LOCK. ADJUSTED THE L1 DOOR INSIDE HANDLE LOCKING HOOK IAW CMM 52- 11-15, AND 52-11-15-400-048-A01.Jun 20, 2018 · N432UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2018062201507Skin · crackedINTERNAL FUSELAGE SKIN AT FRAME 35, STRINGER 30R, HAD A CRACK INDICATION. ACCOMPLISHED A PERMANENT REPAIR IAW PART 3, ECRA 5331-02229.Jun 20, 2018 · N455UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2018062201506Retainer · damagedL1 DOOR SEAL HAD ELONGATED SCREW HOLES. REMOVED AND REPLACED UPPER RETAINER IAW AMM-52-11-18-400-001-A, 52-11-18-110-050-A.Jun 20, 2018 · N455UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018062201505Door Seal · wornL1 DOOR SEAL WAS WORN BEYOND LIMITS. REMOVED AND REPLACED THE L1 DOOR SEAL IAW AMM 52-11-18-400-001-A.Jun 20, 2018 · N455UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2018062201504Door Frame · corrodedR1 DOOR LOWER FWD CORNER HAD AN AREA OF CORROSION ON THE CUTOUT. REPAIRED THE R1 DOOR IAW ECRA 5311-01954.Jun 20, 2018 · N455UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018062201503Stringer · corrodedCORROSION ON STRINGER 41R, IN THE FWD CARGO BILGE AREA. APPROXIMATLY 6 INCHES AFT OF FRAME 30. AFTER BLENDING OF THE STRINGER, FOUND OUT OF LIMITS. REMOVED THE DAMAGED STRINGER SECTION, HFEC AND ROTO PROBED PERFORMED. NO DEFECTS NOTED. REPLACED THE STRINJun 20, 2018 · N455UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR GTIA2018062127007Unknown · odorFUME EVENT IN THE MID CABIN, DURING SHORT FINAL. F/A REPORTED A MUSTY ODOR IN THE MID CABIN ONLY. CHECKED ENGINE DE-OILERS & APU FOR LEAKS, NO FAULTS NOTED. PERFORMED IDENTIFICATION OF THE CAUSE OF ODOR IN CABIN IAW TSM 05-50-00-810-831-A. PERFORMED ENGINJun 20, 2018 · N602NK · Airbus A320232 · Air Distribution System
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